Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences (2016)
- Authors:
- USP affiliated authors: MUÑOZ, HERNAN DARIO CERON - EESC ; ABDALLA, ALVARO MARTINS - EESC ; CATALANO, FERNANDO MARTINI - EESC
- Unidade: EESC
- Subjects: TÚNEIS DE VENTO; AERODINÂMICA DE AERONAVES; ASAS DE AERONAVES; ENGENHARIA AERONÁUTICA
- Language: Inglês
- Imprenta:
- Publisher: Swedish Society of Aeronautics and Astronautics
- Publisher place: Stockholm, Sweden
- Date published: 2016
- Conference titles: Aerospace Technology Congress
-
ABNT
CATALANO, Fernando Martini et al. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016, Anais.. Stockholm, Sweden: Swedish Society of Aeronautics and Astronautics, 2016. . Acesso em: 24 abr. 2024. -
APA
Catalano, F. M., Abdalla, A. M., Cerón Muñoz, H. D., & Munjulury, R. C. (2016). Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. In . Stockholm, Sweden: Swedish Society of Aeronautics and Astronautics. -
NLM
Catalano FM, Abdalla AM, Cerón Muñoz HD, Munjulury RC. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016 ;[citado 2024 abr. 24 ] -
Vancouver
Catalano FM, Abdalla AM, Cerón Muñoz HD, Munjulury RC. Experimental aerodynamic analysis of a fighter aircraft with a canard, forward swept wing and dorsal intake operating at high incidences. 2016 ;[citado 2024 abr. 24 ] - Aerodynamic analysis of the influence of canopy shape in the supersonic dorsal intake design
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